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RADIOFREQUENCY TRANSMISSION CHARACTERISTICS OF CANDIDATE ABLATION MATERIALS FOR PLANETARY-ENTRY-VEHICLE HEAT SHIELDS.

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BookPublisher: Nasa, Washington, D.C. 1968Description: 60.DDC classification: NASA | TN D-4920

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-4920 (Browse shelf)	Not for loan		TR11380

Total holds: 0

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Previous	NASA TN D-4917 COMPUTE--A TIME-SHARING DESK CALCULATOR PROGRAM.	NASA TN D-4918 POINT DEFFECT CALCULATIONS IN TUNGSTEN.	NASA TN D-4919 THE PATH OF A JET DIRECTED AT LARGE ANGLES TO A SUBSONIC FREE STREAM.	NASA TN D-4920 RADIOFREQUENCY TRANSMISSION CHARACTERISTICS OF CANDIDATE ABLATION MATERIALS FOR PLANETARY-ENTRY-VEHICLE HEAT SHIELDS.	NASA TN D-4922 URANIUM DIOXIDE VENT LOSS IN AN EXTERNALLY FUELED THERMIONIC REACTOR CONCEPT	NASA TN D-4923 THE EFFECTS OF REACTOR RADIATION ON 22-VOLT SILICON VOLTAGE REGULATOR DIODES	NASA TN D-4924 ACCEPTANCE TESTING LUNAR AND PLANETARY VEHICLES	Next

Bound With Nasa Tn D-4911-19

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